View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63249U 26145.25066748 +.00000000 +00000-0 +38821-3 0 00008
2 63249 97.6907 37.6805 0001453 330.4265 29.6874 14.97092361 07
| Epoch (UTC): | 25 May 2026 06:00:57 |
| Eccentricity: | 0.0001453 |
| inclination: | 97.6907° |
| perigee height: | 575 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 37.6805° |
| argument of perigee: | 330.4265° |
| revolutions per day: | 14.97092361 |
| mean anomaly at epoch: | 29.6874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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